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1 The Angara rocket family is a family of space-launch vehicles currently under development by the Khrunichev State Research and Production Space Center. The rockets, which are to provide lifting capabilities between 2,000 and 40,500 kg into low earth orbit, are intended to become the mainstay of the Russian unmanned launcher fleet in the future and replace several existing systems. The Angara rockets have a modular design similar to the EELV, based on a common Universal Rocket Module (URM). Depending on configuration, the first stage can consist of 1, 3, 5 or 7 such modules. Unlike EELV launchers, Angara will not employ solid rocket boosters (SRB). The URM is a wholesome structure that includes an oxidizer tank, a fuel tank and a propulsion bay. Each URM will have one single-chamber RD-191 engine (Lox/kerosene). The RD-191 design is based on the RD-170 four-chamber engine used by the Energia launcher, as well as on the RD-171, which is currently used by the Zenit rocket. The first stage of Angara 5 can consist of 5 URM. The second stage will be Block I (also called URM-2), which is powered by the RD-0124A engine. Angara 5 will use the Breeze-M upper stage (currently used for the Proton-M rocket) or KVRB (Lox/LH2). Most versions are intended for unmanned launches, but Angara A5P and Angara A7P are being designed to be capable of launching manned spacecraft. A single launch pad can be used for launching all Angara versions. (from H ~ 580 mm Paper used: 0,26 mm gr ("cardstock") 0,15 mm gr Glue: PVA

2 D31b D2 D31c D0 D2a D2 D1 D31a D31 D31 for D31 Page 2 print on cardstock

3 D32a D32 D31 D32 for D32 D32-1 D32-1 D32-1 D32-1 D32-2 D32-2 D32e D32 D32d D32d-1 D4 D5 for D32d D32b D32c D32d-1 Page 3 print on cardstock

4 D5 D32-2 D32-2 D32-4 D32-4 D32-4 D32-4 for D5 D5b D5 D5c D5a C1 C2 for D5c C2a D4 C1 D5a C2b option glue onto cardstock C2 glue onto cardstock slots option C2e C2e for C2 C2c C2 Page 4 print on cardstock

5 B1 B22b B22c B21a B21b C2d B1 B21 C2b bottom edge of C2 B21 slots holes for A0 B21c for B21 B21c B21c for C2d Page 5 print on cardstock

6 B22 B21d B22a B21 B22 slots holes for A0 B22d B4 B22e B22c B3 B4 B4b B3 for B4 for B22 B22 for B22e B22g-2 B22g B22g-1 B22g-2 B22g-1 B4d B4d-1 B4d-1 B4a B4c Page 6 print on cardstock

7 A1 A1c A1b A1 A1a d=4,5 mm slots A1b A21 A21a A21 hole for A0 A21b A21c for A21 A22b A22e A22a A21 A22 Page 7 print on cardstock 4 copies

8 A22 slots holes for A0 for A22 A22d A22 A22f A22f-1 A22f-1 Page 8 print on cardstock 4 copies

9 B22g-1 B21c B22g B22g-1 B22g-2 B22g-2 C2e / / / / s B21c/ Page 9 print on fine paper

10 spare D32-2 D32-1 D32-1 D32-2 D32-2 D32-5 D32-4 rods for assembling blocks of stage A with stage B A0 (x 12) d=1,5mm L=10mm B4e-1 D32-5 (x 4) rod d=1 mm L=8 mm D32-4 D32-4 B4e-1 / nozzle insertion A22h-1 A22h-1 / A22h-2 A22h-2 A22h-1 A22h-1 / A22h-2 A22h-2 A22h-1 A22h-1 / A22h-2 A22h-2 A22h-1 A22h-1 / A22h-2 A22h-2 Page 10 print on fine paper

11 D0 D1 Assembly diagram D2a D2 D31a D31b A1a A1 stage 1 (URM-1 x 4 + core URM-1) C2 B1 D31 A1c A1b A21a A21b A0 C2d 15 mm B21a B21d Fairing D31c D32a A21 B21 D32-1 D32b B21c D32 Page 11 D32-2 D32-5 D32-4 stage 3 (Breeze-M) stage 2 (Block I) D32c D32d-1 D32d D32e D4 D5 D5a D5b D5c C1 C2a C2 C2e C2b C2c B1 C2d A21c A22a A22b A22 A22d A22e A22f A22h-1 A22h-2 A0 1 mm nozzle insertion B21b B22a B22b B22 B22g B22c B22d B3 B22e B4a B4 B4b B4c B4d B4e-1

12 stage 2 stage 1 (core URM-1) Assembly steps of Fairing, stage 3 (Breeze-M), stage 2 (Block I) and stage 1 (core URM-1) Fairing A1 A2 D32c D32d-1 stage 3 D5a A2 C2 A1 C2c C2a C2b A D32 D32e A D5 D5b A B C2d B21 D32d B D5c B C B22 C C B1 D4 C1 B22e A B4 Page 12

13 Top view D1, D2 D32-2 A1 D32-1 Bottom view B22g B4e C2e A0 A22h Page 13

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